No fatalities

2006-02-03: De Havilland DH.104 Dove (ZK-UDO) — Private New Zealand — Ohakea AFB (Bulls), New Zealand

Ohakea AFB (Bulls), New ZealandLanding (descent or approach)

On February 3, 2006, a De Havilland DH.104 Dove (registration ZK-UDO) operated by Private New Zealand was involved in an aviation accident near Ohakea AFB (Bulls), New Zealand during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: Failure of the port flap jack linkage eye-bolt which caused an asymmetrical flap condition, causing the aircraft to be out of control. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781199075Data APIEditorial standards

A private tour aircraft diverted to Ohakea AFB due to weather. On final approach, full flap selection caused uncontrolled roll. The aircraft struck the runway and was damaged beyond repair; all occupants were uninjured.

Incident Overview

A private tour aircraft diverted to Ohakea Air Force Base (AFB) after encountering deteriorating weather conditions en route. During the final approach, the crew selected full flaps, which resulted in the aircraft rolling left and right. The pilots were unable to maintain control, and the aircraft struck the runway surface before coming to rest. While all occupants escaped without injury, the aircraft sustained damage that rendered it beyond economical repair.

Aircraft Control Issues

The loss of control occurred when full flaps were deployed. The crew experienced an uncommanded roll motion, alternating left and right, which prevented them from stabilizing the aircraft for landing. The aircraft subsequently impacted the runway, coming to a stop on the runway surface.

Occupant Status

All occupants aboard the aircraft were uninjured in the incident.

Damage Assessment

Following the impact, the aircraft was evaluated and found to be damaged beyond repair. No further details on specific structural or system damage were provided.

Official Finding

The investigation identified a mechanical failure as the cause of the loss of control. Specifically, the port flap jack linkage eye-bolt failed, leading to an asymmetrical flap condition. This asymmetry made the aircraft uncontrollable during the landing flare.

Probable cause

Failure of the port flap jack linkage eye-bolt which caused an asymmetrical flap condition, causing the aircraft to be out of control.